View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 51949U 22023D 25316.87169271 .00005205 00000-0 22631-3 0 9994
2 51949 63.4581 286.9752 0107553 350.7221 9.1901 15.18455301204871
| Epoch (UTC): | 12 November 2025 20:55:14 |
| Eccentricity: | 0.0107553 |
| inclination: | 63.4581° |
| perigee height: | 436 km |
| apogee height: | 584 km |
| right ascension of ascending node: | 286.9752° |
| argument of perigee: | 350.7221° |
| revolutions per day: | 15.18455301 |
| mean anomaly at epoch: | 9.1901° |
| orbit number at epoch: | 20487 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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